View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63706U 26145.42346111 +.00000000 +00000-0 +79991-3 0 00003
2 63706 53.1599 223.4355 0001382 89.3559 270.7600 15.30203315 08
| Epoch (UTC): | 25 May 2026 10:09:47 |
| Eccentricity: | 0.0001382 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.4355° |
| argument of perigee: | 89.3559° |
| revolutions per day: | 15.30203315 |
| mean anomaly at epoch: | 270.7600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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